SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG. Integrated Avionics System Garmin G1000,

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1 DA 40 NG AFM Garmin G1000, P-RNAV Operation SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG Integrated Avionics System Garmin G1000, Doc. No. : E Date of Issue : Design Change Advisory : OÄM This Supplement to the Airplane Flight Manual is EASA approved under Approval Number DIAMOND AIRCRAFT INDUSTRIES GMBH N.A. OTTO-STR. 5 A-2700 WIENER NEUSTADT AUSTRIA 9-A33-1

2 Garmin G1000, DA 40 NG AFM Intentionally left blank. Page 9-A33-2 Rev. 0 Doc. # E

3 DA 40 NG AFM Garmin G1000, 0.1 RECORD OF REVISIONS Rev. No. Reason Chapters Page(s) Date of Revision Approval Note Date of Approval Date Inserted Signature 1 Correction 0, 2 9-A33-03, 9-A33-04, 9-A Aug-2011 Rev. 1 to AFM Supplement A33 to AFM Doc. No E is approved under the authority of DOA No. EASA 21J Aug AFM Revision 3 0, 1 9-A33-03, 9-A33-04, 9-A Jul-2014 Rev. 2 to AFM Supplement A33 to AFM Doc. No E is approved under the authority of DOA No. EASA 21J Jan-2015 Doc. # E 01-Jul-2014 Rev. 2 Page 9-A33-3

4 Garmin G1000, DA 40 NG AFM 0.2 LIST OF EFFECTIVE PAGES Chapter Page Date A A A A A A A A33-8 EASA approved 9-A33-9 EASA approved 9-A33-10 EASA approved 9-A33-11 EASA approved 9-A33-12 EASA approved 9-A Jul Jul Jul Aug A A 9-A B 9-A , 6, 7, 8 9-A33-14 Page 9-A Jul-2014 Rev. 2 Doc. # E

5 DA 40 NG AFM Garmin G1000, 0.3 TABLE OF CONTENTS 1. GENERAL... 9-A OPERATING LIMITATIONS... 9-A EMERGENCY PROCEDURES... 9-A A. NORMAL OPERATING PROCEDURES... 9-A B. ABNORMAL OPERATING PROCEDURES... 9-A PERFORMANCE... 9-A MASS AND BALANCE... 9-A DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS... 9-A AIRPLANE HANDLING, CARE AND MAINTENANCE... 9-A33-14 Doc. # E Rev. 0 Page 9-A33-5

6 Garmin G1000, DA 40 NG AFM 1. GENERAL 1.5 DEFINITIONS AND ABBREVIATIONS (i) Miscellaneous AC: AMC: AIRAC: SBAS: WAAS: EGNOS: MSAS: RNAV: P-RNAV: B-RNAV: LPV: LNAV/VNAV: LNAV+V: RNP: GNSS: STAR: SID: ETSO: RAIM: WFDE: Advisory Circular Acceptable Means of Compliance Aeronautical Information Regulation and Control Satellite Based Augmentation System Wide Area Augmentation System European Geostationary Navigation Overlay Service Multi-functional Satellite Augmentation System Area Navigation Precision Area Navigation Basic Area Navigation Localizer Performance with Vertical Guidance Lateral Navigation / Vertical Navigation Lateral Navigation with Advisory Vertical Guidance Required Navigation Performance Global Navigation Satellite System Standard Terminal Arrival Route Standard Instrument Departure European Technical Standard Order Receiver Autonomous Integrity Monitoring WAAS Fault Detection/Exclusion Page 9-A33-6 Rev. 0 Doc. # E

7 DA 40 NG AFM Garmin G1000, G1000 AVIONICS SYSTEM The Garmin GNSS navigation system installed in this airplane is a GPS system with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145a Class 3 approved Garmin GIA 63Ws, TSO-C146a Class 3 approved Garmin GDU 104X Display Units, Garmin GA36 antennas, and GPS/WAAS software version 3.1 or later approved version. The Garmin GNSS navigation system in this airplane is installed in accordance with FAA AC B, EASA AMC and EASA NPA 2009 (AMC 20-28). NOTE The following listing of the Garmin G1000 operational capabilities does not constitute an operational approval. For the operational approval of the airplane contact the appropriate governing authority. The Garmin GNSS navigation system as installed in this airplane complies with the requirements of FAA AC B, EASA AMC and EASA AMC and is approved for navigation using GPS and SBAS (within the coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR enroute, terminal area, and non-precision approach operations (including those approaches titled GPS and RNAV (GPS) approaches). The Garmin GNSS navigation system installed in this airplane is approved for approach procedures with vertical guidance including LPV, LNAV/VNAV and LNAV+V, within the European and U.S. National Airspace System. The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC and meets the equipment performance and functional requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures without RF (radius to fix) legs. Doc. # E 01-Jul-2014 Rev. 2 Page 9-A33-7

8 Garmin G1000, DA 40 NG AFM The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements of FAA AC A for RNAV 2 and RNAV 1 operations. The Garmin GNSS navigation system as installed in this airplane has been found to comply with the requirements for primary means of Class II navigation in oceanic and remote navigation (RNP-10) without time limitations in accordance with FAA AC B and FAA Order A. The Garmin GNSS navigation system can be used without reliance on other long-range navigation systems. The Garmin GNSS navigation system as installed in this airplane has been found to comply with the navigation requirements for primary means of Class II navigation in oceanic and remote navigation (RNP-4) in accordance with FAA AC B and FAA Order The Garmin GNSS navigation system can be used without reliance on other long-range navigation systems. Additional equipment may be required to obtain operational approval to utilize RNP-4 performance. The Garmin GNSS navigation system as installed in this airplane complies with the accuracy, integrity, and continuity of function, and contains the minimum system functions required for PRNAV operations in accordance with JAA Administrative & Guidance Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1). The GNSS navigation system has two ETSO-145 / TSO-C145a Class 3 approved Garmin GIA 63Ws, and ETSO-146 / TSO-C146a Class 3 approved Garmin GDU 104X Display Units. The Garmin GNSS navigation system as installed in this airplane complies with the equipment requirements for PRNAV and BRNAV operations in accordance with FAA AC 90-96A and JAA TGL-10 Rev 1 and AMC Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with FAA AC for database Integrity, quality, and database management practices for the Navigation database. Pilots and operators can view the LOA status at > Aviation Databases > Type 2 LOA Status. Navigation information is referenced to WGS-84 reference system. Page 9-A33-8 Rev. 0 Doc. # E

9 DA 40 NG AFM Garmin G1000, 2. OPERATING LIMITATIONS 2.16 OTHER LIMITATIONS G1000 GPS NAVIGATION SYSTEM LIMITATIONS NOTE The following set of limitations supersedes the limitations addressing the same functions of the G1000 in the basic AFM limitation section. All other Garmin G1000 Avionic System limitations remain effective. The following placard is no longer applicable: GPS NOT APPROVED FOR WAAS OPERATIONS Flight Preparation Phase For flight planning purposes, operations on RNP and RNAV procedures when SBAS signals are not available, the availability of GPS integrity RAIM shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met. For flight planning purposes for operations within European B-RNAV and P-RNAV airspace, if more than one satellite is scheduled to be out of service, then the availability of GPS integrity RAIM shall be confirmed for the intended flight (route and time). In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met. Doc. # E EASA approved Rev. 0 Page 9-A33-9

10 Garmin G1000, DA 40 NG AFM For flight planning purposes, operations where the route requires Class II navigation the airplane s operator or pilot-in-command must use the Garmin WFDE Prediction program to demonstrate that there are no outages on the specified route that would prevent the Garmin GNSS navigation system to provide primary means of Class II navigation in oceanic and remote areas of operation that requires (RNP-10 or RNP-4) capability. If the Garmin WFDE Prediction program indicates fault exclusion (FDE) unavailability will exceed 34 minutes in accordance with FAA Order A for RNP-10 requirements, or 25 minutes in accordance with FAA Order for RNP-4 requirements, then the operation must be rescheduled when FDE is available. NOTE Within the United States, RAIM availability can be determined using the Garmin WFDE Prediction program 3.00 or later approved version with Garmin GA36 antennas selected, or the FAA s enroute and terminal RAIM prediction website: or by contacting a Flight Service Station. NOTE Within Europe, RAIM availability can be determined using the Garmin WFDE Prediction program or Europe s AUGER GPS RAIM Prediction Tool at augur/app/home. For other areas, use the Garmin WFDE Prediction program. This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of flight. The route planning and WFDE prediction program may be downloaded from the GARMIN website on the internet. For information on using the WFDE Prediction Program, refer to GARMIN WAAS FDE Prediction Program, part number , WFDE Prediction Program Instructions. Navigation information is referenced to WGS-84 reference system, and should only be used where the Aeronautical Information Publication (including electronic data and aeronautical charts) conform to WGS-84 or equivalent. Page 9-A33-10 EASA approved 16-Aug-2011 Rev. 1 Doc. # E

11 DA 40 NG AFM Garmin G1000, For flight planning purposes, it is not acceptable to plan a RNAV (GPS) LPV or LNAV/VNAV approach on the destination and alternate airport. The alternate airport must be planned using a LNAV approach or available ground-based aid. Preflight Phase SBAS functionality must be enabled on the G1000 GPS Status page (refer to the G1000 Pilot s Guide for procedure). The pilot must confirm at system initialization that the Navigation database is current. GPS/SBAS based IFR enroute, oceanic, and terminal navigation is prohibited unless the pilot verifies and uses a valid, compatible, and current Navigation database or verifies each waypoint for accuracy by reference to current approved data. Navigation database is expected to be current for the duration of the flight. If the AIRAC cycle will change during flight, the pilot must ensure the accuracy of navigation data, including suitability of navigation facilities used to define the routes and procedures for flight. If an amended chart affecting navigation data is published for the procedure, the database must not be used to conduct the procedure. NOTE Discrepancies that invalidate a procedure must be reported to Garmin International. The affected procedure is prohibited from being flown using data from the Navigation database until a new Navigation database is installed in the airplane and verified that the discrepancy has been corrected. Contact information to report Navigation database discrepancies can be found at > Support > Contact Garmin Support > Aviation. Pilots and operators can view navigation data base alerts at > In the Air > NavData Alerts. Doc. # E EASA approved Rev. 0 Page 9-A33-11

12 Garmin G1000, DA 40 NG AFM Both Garmin GPS navigation receivers must be operating and providing GPS navigation guidance to their PFD for operations requiring RNP-4 performance. North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace operations per FAA AC and FAA AC require both GPS/SBAS receivers to be operating and receiving usable signals except for routes requiring only one Long Range Navigation sensor. In Flight Phase Manual entry of waypoints using latitude/longitude or place/bearing is prohibited. NOTE Whenever possible, RNP and RNAV routes including Standard Instrument Departures (SIDs) and Obstacle Departure Procedures (ODPs), Standard Terminal Arrival (STAR), and enroute RNAV Q and RNAV T routes should be loaded into the flight plan from the database in their entirety, rather than loading route waypoints from the database into the flight plan individually. Selecting and inserting individual named fixes from the database is permitted, provided all fixes along the published route to be flown are inserted. Approach Phase GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Navigation database. NOTE Not all published Instrument Approach Procedures (IAP) are in the Navigation database. Pilots planning on flying an RNAV instrument approach must ensure that the Navigation database contains the planned RNAV Instrument Approach Procedure and that approach procedure must be loaded from the Navigation database into the FMS flight plan by its name. Page 9-A33-12 EASA approved Rev. 0 Doc. # E

13 DA 40 NG AFM Garmin G1000, IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches authorized by the appropriate governing authority. Advisory vertical guidance deviation information is only an aid to help pilots comply with altitude restrictions. When using advisory vertical guidance, the pilot must use the primary barometric altimeter to ensure compliance with all altitude restrictions, particularly during instrument approach operations. The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart. Use of the Garmin GPS/SBAS receivers to provide navigation guidance during the final approach segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for or GPS navigation is prohibited. When using the Garmin VOR/LOC/GS receivers to fly the final approach segment, VOR/LOC/GS navigation data must be selected and presented on the CDI of the pilot flying. Doc. # E EASA approved Rev. 0 Page 9-A33-13

14 Garmin G1000, DA 40 NG AFM 3. EMERGENCY PROCEDURES No changes. 4A. NORMAL OPERATING PROCEDURES No changes. 4B. ABNORMAL OPERATING PROCEDURES No changes. 5. PERFORMANCE No changes. 6. MASS AND BALANCE No changes. 7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS No changes. 8. AIRPLANE HANDLING, CARE AND MAINTENANCE No changes. Page 9-A33-14 Rev. 0 Doc. # E

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